Commercial Aircraft Directory - Aircraft Specification

Airbus - A321-100

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 11 Mar 1993  
Certification date: 17 Dec 1993  

PRINCIPAL DIMENSIONS

Fuselage width: 3.96 m 
Fuselage height: 6 m 
Fuselage length: 44.5 m 
Cabin length: 34.44 m 
Cabin width: 3.7 m 
Cabin height: 2.13 m 
Cabin volume: 155 m3 
Hold volume: 58 m3 

WEIGHTS

Empty operating: 47,603 kg 
Max zero fuel: 67,200 kg 
MTOW: 83,000 kg 
MLW: 71,500 kg 
Standard fuel capacity: 23,700 kg 
Max fuel capacity: 23,700 kg 

SPEEDS

Normal cruise: 811 km/h 
Max cruise: 875 km/h 

PERFORMANCE

Long Range Cruise alt: 10,668 m 
Max ceiling: 12,131 m 
Take off field length: 1,829 m 
Landing field length: 1,600 m 
Max Payload Range: 4,000 m 
Range notes: 1. MTOW options: 85000, 89000, 93500 kg. 2. MLW options: 73500 & 77800 kg. 3. MRW options: 85400, 89400, 93900 kg 4. MZFW options: 69500 & 73000 kg. 5. Max Fuel option: 29680 kg.  
Max passengers: 220  
Typical passengers: 185  

POWERPLANT

Category: Turbofan  
Manufacturer: IAE International Aero Engines  
Model/Submodel: V2530 A5  
Thrust: 140 kN  

MAINTENANCE PROVIDERS

Asiana Airlines Maintenance
Onur Air
TransAsia Airways